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Research on MHD heat shield effect under flight condition

Research Project

Project/Area Number 26820378
Research Category

Grant-in-Aid for Young Scientists (B)

Allocation TypeMulti-year Fund
Research Field Aerospace engineering
Research InstitutionOkayama University

Principal Investigator

NAGATA YASUNORI  岡山大学, 自然科学研究科, 助教 (20635594)

Research Collaborator YUHARA Shota  
MUTA Masayuki  
Project Period (FY) 2014-04-01 – 2017-03-31
Project Status Completed (Fiscal Year 2016)
Budget Amount *help
¥3,900,000 (Direct Cost: ¥3,000,000、Indirect Cost: ¥900,000)
Fiscal Year 2016: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2015: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2014: ¥2,340,000 (Direct Cost: ¥1,800,000、Indirect Cost: ¥540,000)
Keywords航空宇宙工学 / 大気圏再突入機 / プラズマ流制御 / 電磁流体 / 熱防御システム
Outline of Final Research Achievements

MHD heat shield is an innovative technology to protect the vehicle from severe heating during atmospheric entry flight to return from the space. In this research, the MHD heat shield effect was experimentally measured under air plasma flow to improve the numerical prediction. As a result, new measurement device was developed and it was confirmed that the MHD heat shield effect is also generated under the air plasma flow.

Report

(4 results)
  • 2016 Annual Research Report   Final Research Report ( PDF )
  • 2015 Research-status Report
  • 2014 Research-status Report
  • Research Products

    (5 results)

All 2016 2015 2014

All Journal Article (1 results) (of which Peer Reviewed: 1 results,  Acknowledgement Compliant: 1 results) Presentation (4 results) (of which Int'l Joint Research: 1 results)

  • [Journal Article] Drag Enhancement for Atmospheric Entry Capsule using Electrodynamic Effect with Multi-magnetic Source2016

    • Author(s)
      Yasunori NAGATA, Kazuhiko YAMADA, Takashi ABE
    • Journal Title

      TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN

      Volume: 14 Issue: ists30 Pages: Pe_105-Pe_111

    • DOI

      10.2322/tastj.14.Pe_105

    • NAID

      130005180574

    • ISSN
      1884-0485
    • Related Report
      2016 Annual Research Report
    • Peer Reviewed / Acknowledgement Compliant
  • [Presentation] 抗力増大効果に対する磁場印加型模型の形状の影響2016

    • Author(s)
      牟田将之,柳瀬眞一郎,河内俊憲,永田靖典
    • Organizer
      第18回 日本流体力学会 中四国・九州支部講演会
    • Place of Presentation
      岡山
    • Year and Date
      2016-11-26
    • Related Report
      2016 Annual Research Report
  • [Presentation] 極超音速プラズマ気流に対する複数磁場印加による効果2015

    • Author(s)
      永田靖典,柳瀬眞一郎,山田和彦,安部隆士
    • Organizer
      日本機械学会 第28回計算力学講演会
    • Place of Presentation
      横浜
    • Year and Date
      2015-10-11
    • Related Report
      2015 Research-status Report
  • [Presentation] Drag Enhancement for Atmospheric Entry Capsule using Electrodynamic Effect with Multi-magnetic Source2015

    • Author(s)
      Yasunori Nagata, Kazuhiko Yamada, Takashi Abe
    • Organizer
      30th International Symposium on Space Technology and Science
    • Place of Presentation
      Kobe-Hyogo, Japan
    • Year and Date
      2015-07-07
    • Related Report
      2015 Research-status Report
    • Int'l Joint Research
  • [Presentation] 大気圏再突入機の電磁力を用いた抗力増大技術2014

    • Author(s)
      永田靖典
    • Organizer
      第14回日本流体力学会中四国・九州支部講演会
    • Place of Presentation
      岡山大学(岡山県・岡山市)
    • Year and Date
      2014-12-13
    • Related Report
      2014 Research-status Report

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Published: 2014-04-04   Modified: 2018-03-22  

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